Abstract: In this paper, an attempt has been made to study the
effect of thermal gradation on the steady-state creep behavior of
rotating isotropic disc made of functionally graded material using
threshold stress based Sherby’s creep law. The composite discs made
of aluminum matrix reinforced with silicon carbide particulate have
been taken for analysis. The stress and strain rate distributions have
been calculated for the discs rotating at elevated temperatures having
thermal gradation. The material parameters of creep vary radially and
have been estimated by regression fit of the available experimental
data. Investigations for discs made up of linearly increasing particle
content operating under linearly decreasing temperature from inner
to outer radii have been done using von Mises’ yield criterion. The
results are displayed and compared graphically in designer friendly
format for the above said disc profile with the disc made of particle
reinforced composite operating under uniform temperature profile. It
is observed that radial and tangential stresses show minor variation
and the strain rates vary significantly in the presence of thermal
gradation as compared to disc having uniform temperature.
Abstract: The present paper investigates the effect of linear
thermal gradient on the steady-state creep behavior of rotating
isotropic disc using threshold stress based Sherby’s creep law.
The composite discs made of aluminum matrix reinforced with
silicon carbide particulate has been taken for analysis. The stress
and strain rate distributions have been calculated for discs rotating
at linear thermal gradation using von Mises’ yield criterion. The
material parameters have been estimated by regression fit of the
available experimental data. The results are displayed and compared
graphically in designer friendly format for the above said temperature
profile with the disc operating under uniform temperature profile. It is
observed that radial and tangential stresses show minor variation and
the strain rates vary significantly in the presence of thermal gradation
as compared to disc having uniform temperature.
Abstract: Composite laminates are relatively weak in out of
plane loading, inter-laminar stress, stress concentration near the edge
and stress singularities. This paper develops a new analytical
formulation for laminated composite rotating disc fabricated from
symmetric sequential quasi isotropic layers to predict three
dimensional stress and deformation. This analysis is necessary to
evaluate mechanical integrity of fiber reinforced multi-layer
laminates used for high speed rotating applications such as high
speed impellers. Three dimensional governing equations are written
for rotating composite disc. Explicit solution is obtained with
"Frobenius" expansion series. Based on analytical results, there are
two separate zones of three dimensional stress fields in centre and
edge of rotating disc. For thin discs, out of plane deformations and
stresses are small in comparison with plane ones. For relatively thick
discs deformation and stress fields are three dimensional.